View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 19150U 70025PS 24355.82070756 .00013940 00000-0 75441-2 0 9994
2 19150 100.3215 204.1447 0023450 202.1107 157.9050 14.12477327828327
| Epoch (UTC): | 20 December 2024 19:41:49 |
| Eccentricity: | 0.0023450 |
| inclination: | 100.3215° |
| perigee height: | 834 km |
| apogee height: | 868 km |
| right ascension of ascending node: | 204.1447° |
| argument of perigee: | 202.1107° |
| revolutions per day: | 14.12477327 |
| mean anomaly at epoch: | 157.9050° |
| orbit number at epoch: | 82832 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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